|Publication number||US7345693 B2|
|Application number||US 10/717,664|
|Publication date||Mar 18, 2008|
|Filing date||Nov 21, 2003|
|Priority date||Mar 20, 2002|
|Also published as||CA2421105A1, CA2421105C, DE60330416D1, EP1347412A1, EP1347412B1, US6927782, US7230632, US20030179215, US20040160354, US20040201596|
|Publication number||10717664, 717664, US 7345693 B2, US 7345693B2, US-B2-7345693, US7345693 B2, US7345693B2|
|Inventors||Pierre Coldefy, Fabien Fetzmann, Frederic Lemoult|
|Original Assignee||Airbus France|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (15), Non-Patent Citations (3), Referenced by (24), Classifications (17), Legal Events (4)|
|External Links: USPTO, USPTO Assignment, Espacenet|
This application is a continuation application of U.S. application Ser. No. 10/214,391, filed on Aug. 8, 2002, which claims priority under 35 U.S.C. § 119 to French Patent Application 02 03473, filed on Mar. 20, 2002, the entire contents of both which are incorporated by reference.
1. Field of the Invention
The present invention relates to an airport display device.
2. Discussion of the Background
The complexity of certain airports, the increase in air traffic and the existence of installations that are often poorly adapted to aircraft that are increasingly large and numerous create traffic difficulties on the runways and taxiways of airports, which often give rise to lengthening of the taxiing times, and sometimes to more or less serious incidents and, unfortunately, also to accidents.
In this context, an increasingly high number of “runway incursions” is observed, that is to say situations in which an unauthorized aircraft (or another moving object such as a technical vehicle of the ground support personnel, for example) moves onto a runway which is being used at the same time in a regular manner by another aircraft in order to land or take off. Such a runway incursion is very dangerous, since it puts the lives of the occupants of both aircraft in danger.
For safety reasons, it is therefore important, or even imperative, that each pilot can observe the environment around his aircraft in the most efficient way possible.
Through the document EP-0 980 828, a system is known which is installed on an aircraft in order to assist the pilot of the aircraft during ground maneuvers. For this purpose this system includes a first video camera that generates video images of the forward landing gear and of an area around the latter, a second video camera which generates video images of the main landing gears and of the areas around the latter, and display means that are fitted in the piloting position and which display the video images generated by the the first and second video cameras (which are fixed to the fuselage).
This known system therefore provides the pilot with information that enables him to make maneuvers during a taxiing operation with increased safety. In particular, by observation of the landing gears and of the areas around the latter, he can prevent a landing gear from striking an obstacle on the ground or which does not leave the runway or taxiway on which the aircraft is moving.
However, this known system does not provide any information on the whole (or at least on an extended area) of the runway or of the taxiway. Now, such a lack of information can be dangerous, particularly in poor visibility (fog, etc). In fact, another moving object, in particular another aircraft, can be on the same runway (or the same taxiway) at the same time and, due to lack of information, a situation can arise in which a collision cannot be avoided, in particular if the other moving object is moving at very high speed such as occurs during the take off or landing of an aircraft for example.
The system described in the document EP-0 980 828 also has other disadvantages, in particular the fact that the angles of view are not optimal. The result of this is that the perspective views displayed by this known system has blind spots, for example under the wings where the main landing gear of the aircraft is not seen (the position of the latter only being symbolized) and neither is the possible border of the taxiway or of the runway.
Furthermore, a display system making it possible to partially overcome the above disadvantages is known from an article by Beskenis, Green, Hyer and Johnson entitled “Integrated Display System for Low Visibility Landing and Surface Operations” which appeared in the publication “NASA Langley Technical Report,” July 1998, NASA/CR-1998-208446. This display system includes, in particular, display means making it possible to exhibit on a screen mounted in the piloting position of the aircraft a map of the airport showing the runways, the taxiways and the various buildings, as well as the position of the aircraft and the traffic existing on that airport. This known system furthermore includes an actuating means allowing the pilot to choose between an overall view of the airport in planview and various perspective views of a part of the airport, which have various different degrees of zoom (that is to say different scales).
Even though it thus presents the pilot with a view of the airport with the corresponding traffic, which allows the pilot to form an idea of the real situation, this known system has several disadvantages. In particular, it is a frozen system and is not adaptable to different airports. Furthermore, the presentation of data used by this system is not very legible.
In fact, with this known system, the various displays offered are always the same no matter which airport is being used. Now, airports can of course be of very different sizes, of variable complexities and can include buildings in different quantities and sizes. Consequently, a presentation of information that is adapted to a particular type of airport (small size and few runways and buildings for example) is not generally adapted to another (very large and complex with numerous runways for example), and nothing in this known system makes it possible to take account of such different characteristics.
Furthermore, the presentation of information is not very legible, in particular because of the high number of elements (runways, taxiways, buildings, traffic, etc.) that is present on the display screen, particularly when the degree of zoom is low (a complete view of the airport for example). The legibility is also reduced by the use of different types of views: perspective views, plan views. Thus the pilot always needs a certain amount of time to understand the new display correctly when there is a change of type of view, this loss of time of course being a nuisance in certain situations.
The purpose of the present invention is to overcome these disadvantages. It relates to an airport display device allowing a highly legible display and adaptable to different characteristics (size, complexity, etc.) of the airport.
For this purpose, according to the invention, the display device of the type includes:
at least one display means having at least one display screen;
at least one database containing data relating to the airport;
an actuating system making it possible for an operator to select a degree of zoom for the airport to be displayed, from among a plurality of different degrees of zoom; and
a central unit which is connected to the said display means, to the data base and to the actuating system and which controls the display means such that it exhibits on the display screen at least a part of the airport, and that it does so according to a scale value that is representative of a degree of zoom selected by the intermediary of the actuating system,
is noteworthy in that it furthermore includes at least one means making it possible for an operator to parameterize at least certain of the scale values that are of the type that can be parameterized, in that the display means exhibits the part of the airport solely in plan view on the display screen, and in that the central unit controls the display means such that it exhibits details of the airport on the display screen, according to one of a plurality of different levels of detail, each of the levels of detail being dependent at least on the selected degree of zoom.
Thus, because of the invention, at least certain of the scale values (relating to different degrees of zoom) can be parameterized, which makes it possible in particular to adapt these scale values to the characteristics (size, complexity, etc) of the airport to be displayed.
Furthermore, by the possible adaptation of the level of details that are displayed to the selected degree of zoom (or scale value), it is possible to choose a level of details which makes it possible to display the greatest possible amount of details by overloading the display screen. This therefore makes it possible to make the presentation of information very legible. Of course, according to the invention, when the degree of zoom increases (that is to say with the part of the airport shown on the display screen becomes smaller), the level of detail increases (that is to say new information (or details) is added to the display screen).
The legibility is also increased by the presentation of the views (of part of or all of the airport) exclusively in plan view. Thus, the pilot does not have to recognize a new type of presentation when there is a change of view. Furthermore, a plan view makes it possible to assess easily the distances between the various elements of the airport and to gain a good understanding of the relative disposition of these elements, in particular in comparison with a perspective view.
Furthermore, the actuating system advantageously includes:
at least one first actuating means making it possible (for an operator) to modify (continuously or step by step) the selected degree of zoom, in both directions, between two limit degrees; and/or
at least one second actuating means making it possible (for an operator) to select directly one of at least three different degrees of zoom, respectively relating to:
proximity navigation; and
In this way, the operator can have direct access to preferred degrees of zoom; and/or
at least one third actuating means making it possible (for an operator) to control, by the intermediary of the central unit, the display means in such a way that it automatically centers the part of the airport that it is showing on the display screen on a characteristic sign illustrating the position of a moving object, in particular an aircraft, provided with the display device; and/or
at least one fourth actuating means making it possible (for an operator) to control, by the intermediary of the central unit, the display means such that it centers the part of the airport that it is showing on the display screen on predefined points of the airport, in a cyclic manner, while modifying the view at each new actuation of the fourth actuating means.
In a preferred embodiment, the actuating system furthermore includes at least one fifth actuating means making it possible (for an operator):
starting from a first degree of zoom, to gain access, by a first actuation of the fifth actuating means, to a second degree of zoom allowing a presentation of the whole of the airport on the display screen; and
starting from this second degree of zoom, to return, by a second actuation of the fifth actuating means, to the first degree of zoom.
The return is generally made to the same part of the airport that was shown before the display of the whole of the airport.
However, in a particular preferred embodiment, the actuating system furthermore includes at least one sixth actuating means making it possible (for an operator) to select a point of the airport upon which the part of the airport which is shown on the display screen is then centered. Thus, the return (to the first degree of zoom) can take place on a new part of the airport that has been selected previously, using this sixth actuating means.
Furthermore and advantageously, the display device according to the invention includes a means making it possible to displace the part of the airport that is displayed on the display screen.
Furthermore, in a preferred embodiment, the central unit is made:
such that a variation of zoom between two different degrees of zoom appears continuous to an operator looking at the display screen; and/or
such that a displacement of the part of the airport that is displayed on the display screen appears continuous to an operator looking at the display screen.
Thus, a (visually) continuous transformation of the airport (or of the part of the airport) that is displayed on the screen is obtained, which of course is advantageous with regard to the legibility of the presentation of information.
Furthermore, with the same objective, when the display means includes at least two different display modes, as is the case for a navigation screen of the ND (“Navigation Display”) type for example, the central unit is made such that, during a change of mode from a first mode to a second mode, it successively causes on the display screen at least the disappearance of a mask relating to the first mode, a displacement of the aircraft part that is displayed and the appearance of a mask relating to the second mode.
According to the invention, the following elements in particular are shown on the display screen: the runways, the taxiways, the buildings, . . . , and the traffic (aircraft, etc.). Also, to be able to display the traffic in real time, the display device advantageously furthermore includes means making it possible to load data (in particular that relating to traffic) in real time into the data base which is therefore of the dynamic type.
Furthermore and advantageously:
in a first embodiment, the display device is integrated in a portable computer; and
in a second embodiment, the display means is a display system of an aircraft to which the device according to the invention is fitted, and the elements of the device, other than the display means, form part of a specific assembly.
A more complete appreciation of the invention and many of the attendant advantages thereof will be readily obtained as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings, wherein:
The device 1 according to the invention and shown diagrammatically in
The device 1 is of the type includes:
at least one display means 2 having at least one display screen 3 of normal type;
at least one data base 4 provided with data relating to the airport, which it can receive for example by a link 37;
an actuating system 5 making it possible for an operator to select a degree of zoom for the airport to be displayed, from among a plurality of degrees of zoom; and
a central unit 6 which is connected by the intermediary of links 7, 8 and 9 to the display means 2, to the data base 4 and to the actuating system 5 respectively and which controls the display means 2 such that it shows on the display screen 3 at least a part of the airport according to a scale value representative of a degree of zoom which has been selected by the intermediary of the actuating system 5.
According to the invention:
at least certain of the scale values can be parameterized, and the display device 1 furthermore includes a means 10 which is connected by a link 11 to the central unit 6 and which makes it possible for an operator to parameterize the said scale values that can be parameterized. These means 10 can, for example, be a numerical keypad allowing an operator to enter new scale values;
the display means 2 shows, on the screen 3, only plan views of the airport (or of a part of the latter); and
the central unit 6 controls the display means 2 such that it presents on the screen 3 a set of details that conforms with one of a plurality of different levels of detail. Each of these different levels of detail depends at least on the degree of zoom that is selected by the intermediary of the actuating system 5. In a particular embodiment, these levels of detail can also depend on other factors such as the position of the aircraft for example. Thus, according to the invention, if an operator selects a new degree of zoom that is such that the displayed zone becomes more restricted, the level of detail increases on the display screen 3, that is to say new information not previously shown is the displayed, and vice-versa of course.
Thus, as at least certain of the scale values (that are associated with different degrees of zoom that can be selected) can be parameterized, it is possible to adapt these scale values to the characteristics (size, complexity, etc.) of the airport to be displayed. It can easily be understood that it is not judicious to use the same scale value (that is to say the same ratio between the shown representation of a length and the corresponding real length) for two airports, one of which is much bigger (for example twice as big) and more complex (more runways, etc.) than the other. Consequently, the display device 1 according to the invention can be adapted to any type of airport, whatever its size or complexity may be in particular.
Furthermore, the exclusive use of plan views to represent the airport provides visual comfort to the pilot and facilitates the reading of the views.
The same applies to the adaptation of the levels of detail to the degrees of zoom (and therefore to the scale values) selected, as can be seen by referring to
runways 13 and 14;
a taxiway 15;
bi-pass taxiways 16, 17, 18 and 19; and
a special sign 20 illustrating the position of the aircraft (equipped with the said device 1) which is located on the runway 13 at the level of the bi-pass taxiway 16.
According to the invention, a level of detail is chosen for each degree of zoom which simultaneously allows easy reading of the information presented on the screen 3 and provides an appropriate density of this information.
Furthermore, as shown in
actuating means 23 and 24 which make it possible for an operator to modify the degree of zoom selected, in the direction of decreasing degrees of zoom for the actuating means 23 and in the direction of increasing degrees of zoom for actuating means 24, and for this to be between two limit degrees of zoom. The scale values corresponding to these two degrees of zoom respectively can be parameterized and therefore be adapted to the characteristics of the airport to be displayed. In the context of the present invention, the actuating means 23 and 24 can modify the degree of zoom either continuously or step by step;
an actuating means 25 for automatically centering the part of the airport 12 that is displayed, about the effective position 20 of the aircraft. It is also possible to make provision for the actuating system 5 to furthermore include at least one actuating means, for example the means 31 represented diagrammatically in
a means 26 making it possible to displace the part of the airport that is displayed on the display screen 3, in all directions.
Furthermore, the actuating system 5 includes three associated actuating means 27, 28 and 29 that make it possible to gain direct access to different degrees of zoom that have in particular been defined according to the operational requirements of the pilots. The displays obtained respectively by actuating the actuating means 27, 28 and 29 are particularly appropriate for helping the pilot respectively during:
general navigation. The corresponding degree of zoom allows a good display of the whole of the airport 12 to be able, on the one hand, to have a better understanding of its complexity and, on the other hand, to display any routing whatsoever in its entirety. It is therefore a matter of strategic navigation;
proximity navigation. The corresponding degree of zoom makes it possible for the pilot to navigate in the short term and to observe many parameters relating to his position, and his close environment. In this case it is a matter of tactical navigation; and
precision taxiing, making it possible to respond to the problems of maneuverability and of positioning of the aircraft 20 on a runway 13, 14, a taxiway 15, a parking place, when approaching a gate or for carrying out a maneuver on a turning area (generally located at the end of a runway to allow large aircraft to turn around).
Of course, as mentioned above, the scale values associated with these different degrees of zoom can be parameterized and can be adapted to the airport in particular.
Furthermore, the actuating system 5 also includes an actuating means 30 which makes it possible:
starting from a first view according to a first degree of zoom, for example the view shown in
starting from this overall view (
In this case, in a particular embodiment illustrated in
This latter function will in particular assist the pilot, if he is lost, to locate himself in the airport 12, to search for a precise point in a graphical manner and to observe the surrounding traffic, if the working degree of zoom makes it possible to observe only a small area of the airport (high degree of zoom).
It will be noted that, according to the invention, on increasing the degree of zoom on changing from
Furthermore, the device 1 according to the invention is designed in such a way as to cause a continuous transformation of the displayed information with no sudden changes of information, for example during a variation of zoom or a change of mode such as described below, to make the presentation of information as legible as possible in such a situation.
To do this, according to the invention, the central unit 6 is made:
such that a variation of zoom between two different degrees of zoom appears continuous to an operator looking at the display screen 3. To do this, it suffices to parameterized a sufficient number of time slots, associated with a sufficiently short self-repetition time of the function, to maintain the visual illusion of continuity. In practice, if the repetition rate exceeds a certain threshold (10 Hz for example), the image is considered to be sufficiently fluid; and
such that a displacement of the part of the airport that is displayed on the display screen 3 appears continuous to an operator looking at the display screen 3.
The central unit 6 is also made in such a way as to cause a continuous transformation of the information displayed during change of mode, when the display means 2 includes a plurality of modes, such as an ND (“Navigation Display”) type navigation screen for example.
It is known that such an ND navigation screen includes the following modes:
a so-called “Rose” mode, in which the aircraft is at the center of the display screen 3. It is fixed and the nose faces upwards. Several concentric circles provide a scale of reference for rapidly and visually measuring distances. The pilot can thus easily locate his aircraft on the map of the airport, which rotates and slides in accordance with the movements carried out;
a so-called “Arc” mode, in which the aircraft is at the bottom of the display screen 3, at the center of several arcs of circle, whose separation corresponds to the selected degree of zoom. The map rotates and slides in accordance with the movements of the aircraft, which remains fixed, as in the “Rose” mode; and
a so-called “Plan” mode. This is therefore a plan view of the airport, oriented towards the North. The aircraft moves over this map, which is fixed. The “Plan” mode also includes a mask which resembles that of the “Rose” mode (it includes circles), but it is a little more detached and separated from the aircraft symbol.
When it includes several modes such as the modes, the display means 2 is controlled, according to the invention, by the central unit 6, in such a way as to implement the following successive operations, during a change of mode (change from a first mode to a second mode):
disappearance of the mask described below, relating to the first mode;
continuous sliding of the map displaying the airport;
appearance and disappearance on the display screen 3 of different elements as they enter or leave the display during the automatic sliding of the map; and
appearance of the new mask relating to the second mode.
It is known that a mask relating to a particular mode usually includes a circular scale (for the masks of the “Rose” and “Plan” modes or a semicircular scale (for the mask of the “Arc” mode), representing headings, and a scale, representing distances, situated on the different arcs of circle composing the masks. The arcs of circle are concentric and distributed in a regular manner. It is possible, by a preferred adjustment, for the operator to be able:
either to fix the diameters of the arcs of circle corresponding to the masks, which involves a modification of the value displayed for the distance depending on the degree of zoom;
or to allow the different arcs of circle to resize themselves such that the displayed value of the scale of distances is an integer value that is simpler to interpret.
The masks are therefore objects that inform the operator on the orientation of the aircraft while associating it with a concept of distance.
It will be noted that the function used by the actuation of the previously described actuating means 30 necessitates special processing, including the following successive steps:
reduction of the degree of zoom down to the minimum degree of zoom;
disappearance of the mask, if it is different from the mask of the “Plan” mode;
appearance of the “Plan” mode mask, if the preceding mode was different; and
continuous displacement of the map displayed on the screen 3 to center the airport on the middle of the screen 3 and thus to display it in its entirety.
Starting from this point:
it is possible to repeat the preceding operations in the reverse order, if the operator wishes to return to the initial display;
it is also possible to carry out the following operations:
recentering, by continuous displacement of the map, on a point selected by the operator; and
increasing the degree of zoom up to the initial degree of zoom (the value recorded at the moment of the initial activation of the function).
Furthermore, if the operator wishes to recenter the image on the aircraft (actuating means 25) or on a characteristic point of the airport (actuating means 31), the device 1 carries out the following operations:
reduction of the degree of zoom down to the appearance of the symbol 20 illustrating the aircraft or of the characteristic point on the screen 3;
continuous displacement of the map to center it on the symbol 20 or on the characteristic point; and
return to the initial value of the degree of zoom.
Furthermore, if the display is not centered on the symbol 20 of the aircraft and the operator wishes to return to the “Arc” or “Rose” mode, the device 1 carries out the following operations:
reduction of the degree of zoom down to the appearance of the symbol 20 on the screen 3;
disappearance of the mask of the “Plan” mode;
continuous displacement of the map to center it on the symbol 20 (centering relating to the desired mode: in the center for the “Rose” mode, at the bottom for the “Arc” mode);
appearance of the new mask; and
return to the initial value of the degree of zoom.
Moreover, the device 1 according to the invention furthermore includes means 34 making it possible to update in real time, in a dynamic manner, the data base 4, as illustrated by a link shown in dotted and dashed line 35 in
In the context of the present invention, the actuating system 5 can be of different types. In particular it can be:
a touch-sensitive screen, each of the actuating means 21 to 31 and 36 then corresponding to a particular (touch) sensitive area;
a keyboard, each of the actuating means 21 to 31 and 36 then representing at least one particular key; or
an assembly formed from a computer type panel and a selector (in particular a roller ball) making it possible to select and confirm the different sensitive areas of the computer panel. Preferably, the selector is a means (roller ball, touchpad, miniature joystick, etc) which is firmly attached to a fixed support.
These different types of actuating system 5 that are fixed make it possible to carry out an easy and accurate actuation of one of the actuating means 23 to 31 and 36, in particular in the presence of aircraft vibrations and/or in conditions where the pilot is stressed.
As mentioned previously, the ground map does not constitute the totality of the data base 4. Dynamic elements are included, such as traffic and information specific to the airline companies using the device 1, by the intermediary of the means 34.
Furthermore and advantageously:
in a first embodiment, the display device 1 is integrated in a portable computer that can be installed in the piloting position of an aircraft; and
in a second embodiment, the display means 2 is a display system (for example a navigation screen of the ND (“Navigation Display”) type of the aircraft in which the device 1 is installed, and the elements 4, 5, 6, . . . of the device 1, other than the display means 2, are part of a specific assembly.
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US4729029||Mar 28, 1986||Mar 1, 1988||Thomson-Csf||Process and apparatus for the insertion of insets into the image supplied by a digital scan converter|
|US6121900 *||Aug 10, 1998||Sep 19, 2000||Alpine Electronics, Inc.||Method of displaying maps for a car navigation unit|
|US6246342 *||Mar 3, 1999||Jun 12, 2001||Siemens Aktiengesellschaft||Man-machine interface for airport traffic control purposes|
|US6314370||Nov 29, 1999||Nov 6, 2001||Ames Maps, Llc||Map-based navigation system with overlays|
|US6353794||Oct 19, 1999||Mar 5, 2002||Ar Group, Inc.||Air travel information and computer data compilation, retrieval and display method and system|
|US6405975||Aug 18, 1998||Jun 18, 2002||The Boeing Company||Airplane ground maneuvering camera system|
|US20020004692||Mar 7, 2001||Jan 10, 2002||Winged Systems Corporation||High accuracy, high integrity scene mapped navigation|
|US20020089549 *||Jan 9, 2001||Jul 11, 2002||Munro James A.||Image having a hierarchical structure|
|US20020116097||Oct 11, 2001||Aug 22, 2002||Block Gerald J.||Method and apparatus for reducing false taws warnings and navigating landing approaches|
|US20030018427 *||Jul 21, 2001||Jan 23, 2003||Tatsuo Yokota||Display method and apparatus for navigation system|
|US20030179215||Aug 8, 2002||Sep 25, 2003||Pierre Coldefy||Airport display device|
|DE3939110A1||Nov 25, 1989||May 31, 1990||Elscint Ltd||Image processing system for medical diagnosis - has zoom facility to locate and display area with improved definition|
|EP0529121A1||Aug 24, 1991||Mar 3, 1993||International Business Machines Corporation||Graphics display tool|
|EP0980828A1||Aug 18, 1999||Feb 23, 2000||The Boeing Company||Airplane ground maneuvering camera system|
|WO2001069585A1||Mar 14, 2001||Sep 20, 2001||Picsurf, Inc.||System and method for efficient transmission and display of image details by re-usage of compressed data|
|1||*||Mapquest 2000, pp. 1-2.|
|2||*||Mapquest, 1999, pp. 1-12.|
|3||NASA/CR-1998-208446, "Integrated Display System for Low Visibility Landing and Surface Operations", Jul. 1998, pp. 1-59.|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US7751947||Mar 31, 2004||Jul 6, 2010||The Boeing Company||Methods and systems for displaying assistance messages to aircraft operators|
|US7813845||Feb 19, 2003||Oct 12, 2010||The Boeing Company||Airport taxiway navigation system|
|US7970502||Mar 30, 2009||Jun 28, 2011||The Boeing Company||Apparatuses and systems for controlling autoflight systems|
|US8082070||Jun 25, 2010||Dec 20, 2011||The Boeing Company||Methods and systems for displaying assistance messages to aircraft operators|
|US8095302 *||Mar 4, 2008||Jan 10, 2012||The Boeing Company||Discrepancy reporting in electronic map applications|
|US8180562||Jun 4, 2008||May 15, 2012||The Boeing Company||System and method for taxi route entry parsing|
|US8386167||Nov 14, 2008||Feb 26, 2013||The Boeing Company||Display of taxi route control point information|
|US8494691||Jan 18, 2011||Jul 23, 2013||The Boeing Company||Apparatuses and methods for displaying autoflight information|
|US8502701 *||Oct 16, 2009||Aug 6, 2013||The Boeing Company||Runway status indicator|
|US8504223||Oct 29, 2008||Aug 6, 2013||The Boeing Company||Systems and methods for presenting and obtaining flight control information|
|US9709420 *||May 20, 2015||Jul 18, 2017||Thales||Reconfiguration of the display of a flight plan for the piloting of an aircraft|
|US20040006412 *||Feb 19, 2003||Jan 8, 2004||Reagan Doose||Airport taxiway navigation system|
|US20050228674 *||Mar 31, 2004||Oct 13, 2005||Gunn Peter D||Methods and systems for displaying assistance messages to aircraft operators|
|US20090062972 *||Oct 29, 2008||Mar 5, 2009||The Boeing Company||Systems and Methods for Presenting and Obtaining Flight Control Information|
|US20090228195 *||Mar 4, 2008||Sep 10, 2009||Andre Lutz||Discrepancy reporting in electronic map applications|
|US20090306887 *||Jun 4, 2008||Dec 10, 2009||The Boeing Company||System and Method for Taxi Route Entry Parsing|
|US20100076628 *||Mar 30, 2009||Mar 25, 2010||The Boeing Company||Apparatuses and methods for displaying autoflight information|
|US20100125403 *||Nov 14, 2008||May 20, 2010||Clark Samuel T||Display of Taxi Route Control Point Information|
|US20100262319 *||Jun 25, 2010||Oct 14, 2010||The Boeing Company||Methods and systems for displaying assistance messages to aircraft operators|
|US20110090096 *||Oct 16, 2009||Apr 21, 2011||Juliana Joo-Hong Goh||Runway Status Indicator|
|US20110125347 *||Jan 18, 2011||May 26, 2011||The Boeing Company||Apparatuses and methods for displaying autoflight information|
|US20140088857 *||Sep 14, 2013||Mar 27, 2014||James Theodore Hollin, JR.||Video-graphic runway activity monitoring system|
|US20150338237 *||May 20, 2015||Nov 26, 2015||Thales||Reconfiguration of the display of a flight plan for the piloting of an aircraft|
|USRE41396||Jun 13, 2008||Jun 22, 2010||The Boeing Company||Method and system for entering and displaying ground taxi instructions|
|U.S. Classification||345/660, 345/661, 345/671, 345/670, 345/629, 345/662, 345/668|
|International Classification||G09G5/02, G08G5/06|
|Cooperative Classification||G08G5/0021, G08G5/065, G08G5/0013, G08G5/025|
|European Classification||G08G5/06E, G08G5/02E, G08G5/00B2, G08G5/00A4|
|May 3, 2004||AS||Assignment|
Owner name: AIRBUS FRANCE, FRANCE
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:COLDEFY, PIERRE;FETZMANN, FABIEN;LEMOULT, FREDERIC;REEL/FRAME:015294/0478
Effective date: 20040122
|May 18, 2011||AS||Assignment|
Owner name: AIRBUS OPERATIONS SAS, FRANCE
Free format text: MERGER;ASSIGNOR:AIRBUS FRANCE;REEL/FRAME:026298/0269
Effective date: 20090630
|Sep 8, 2011||FPAY||Fee payment|
Year of fee payment: 4
|Sep 1, 2015||FPAY||Fee payment|
Year of fee payment: 8